CN110497629A - Pultrusion method and apparatus - Google Patents

Pultrusion method and apparatus Download PDF

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Publication number
CN110497629A
CN110497629A CN201910414118.1A CN201910414118A CN110497629A CN 110497629 A CN110497629 A CN 110497629A CN 201910414118 A CN201910414118 A CN 201910414118A CN 110497629 A CN110497629 A CN 110497629A
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CN
China
Prior art keywords
pultrusion
fiber
along
chosen point
manufacturing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201910414118.1A
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Chinese (zh)
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CN110497629B (en
Inventor
D.S.佩德森
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Siemens Gamesa Renewable Energy AS
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Siemens Gamesa Renewable Energy AS
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Publication of CN110497629A publication Critical patent/CN110497629A/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/88Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/523Pultrusion, i.e. forming and compressing by continuously pulling through a die and impregnating the reinforcement in the die
    • B29C70/524Pultrusion, i.e. forming and compressing by continuously pulling through a die and impregnating the reinforcement in the die the transport direction being vertical
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/521Pultrusion, i.e. forming and compressing by continuously pulling through a die and impregnating the reinforcement before the die
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B15/00Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
    • B29B15/08Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
    • B29B15/10Coating or impregnating independently of the moulding or shaping step
    • B29B15/12Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length
    • B29B15/122Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length with a matrix in liquid form, e.g. as melt, solution or latex
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/525Component parts, details or accessories; Auxiliary operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/525Component parts, details or accessories; Auxiliary operations
    • B29C70/526Pultrusion dies, e.g. dies with moving or rotating parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543Fixing the position or configuration of fibrous reinforcements before or during moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/525Component parts, details or accessories; Auxiliary operations
    • B29C70/527Pulling means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/0005Condition, form or state of moulded material or of the material to be shaped containing compounding ingredients
    • B29K2105/002Agents changing electric characteristics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0003Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular electrical or magnetic properties, e.g. piezoelectric
    • B29K2995/0005Conductive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/082Blades, e.g. for helicopters
    • B29L2031/085Wind turbine blades
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

Abstract

The invention relates to a pultrusion method and device. The invention relates to a method of manufacturing a pultruded strip (50) for an elongated structure. The method comprises the following steps: a pultrusion apparatus (100) is provided which includes at least a pultrusion die (20), through which a plurality of fibers (110) are drawn to be infused in a resin, the conductive properties of selected points (200) being varied along the plurality of fibers (110) upstream of the pultrusion die (20).

Description

Pultrusion method and device
Technical field
The present invention relates to a kind of for manufacturing the pultrusion method and device that are used for the pultrusion item of slim-lined construction.
Background technique
Carbon parts are commonly used in various industrial circles.For example, carbon parts can be used for manufacturing the blade of wind turbine So as to make its be used only glass fiber material manufacture blade compared to it is longer and gentlier.Such carbon parts can usually lead to Cross pultrusion process manufacture.
In having in large-sized construction as wind turbine, conductive component usually requires to be electrically connected to lightning-protection system, Carbon parts including wind turbine blade, because carbon is conductive material.
Carbon profile has some electric conductivity generally along machine direction, but is across fiber, and electric conductivity is much lower.This is especially It is the size design of the insulator due to being arranged on each fiber, very thin insulator is administered to the weak company of the fiber beside it It connects.On a microscopic level, the limit of the size design setting electric conductivity of fiber.As macroscopic result, this is made it difficult to carbon type Material is connected to the lightning protection cable of the lightning protection for wind turbine blade, passes through because the power of thunder and lightning can not move fast enough The profile.
In order to avoid this disadvantage, the electric conductivity improved in profile is important.When the fiber of single profile is crossed in raising When electric conductivity, much simpler connection can also be provided, is selected for ensuring convenient lightning protection.
The solution of problem above can be during manufacturing process using conductive adhesive to improve in profile and Electric conductivity between it.This conductive adhesive can be arranged between the fibers in pultrusion process.Such solution Constitute an inconvenience in that, it is known that conductive adhesive the property poorer than non-conductive adhesive is shown in terms of casting time and adhesive force Matter.
Therefore, there is still a need for provide it is a kind of for manufacture be used for slim-lined construction pultrusion item manufacturing method and apparatus, The electric conductivity of middle pultrusion carbon parts is improved, and without the inconvenience above with reference to known description of the prior art.
Summary of the invention
This needs can be by meeting according to the theme of accompanying independent claim.The dependent claims description present invention Advantageous embodiment.
According to the first aspect of the invention, a kind of method manufacturing the pultrusion item for slim-lined construction is provided.The method The following steps are included:
Pultrusion apparatus is provided, pultrusion die is included at least, multiple fibers are pulled through the pultrusion mould Have to be immersed in resin,
Change the conduction property of Chosen Point along the multiple fiber in pultrusion die upstream.
According to the second aspect of the invention, a kind of pultrusion apparatus is provided, is included at least: pultrusion die, it is more A fiber is pulled through the pultrusion die to be immersed in resin;And rove section (roving section), The rove section is in pultrusion die upstream with the conduction property for changing Chosen Point along the multiple fiber.
Methods and apparatus of the present invention and method solve the inconvenience of the prior art advantageous by following manner: it is logical The conduction property of the Chosen Point of change limited quantity is crossed to improve the electric conductivity of slim-lined construction.This is in the machine for not damaging slim-lined construction The conduction property of slim-lined construction is improved in the case where tool property.
According to an embodiment of the invention, being implemented by the drop for injecting or depositing conductive adhesive along the multiple fibre Dimension changes the conduction property of Chosen Point.This can be used for by being provided with the rove section for the pultrusion apparatus being defined above The one or more nozzles of drop for injecting at Chosen Point along the multiple fiber or depositing conductive adhesive are realized.
According to an embodiment of the invention, implementing to change Chosen Point along the multiple fiber by the size for changing fiber Conduction property.In particular, it can press or squeeze to change size or the surface of fiber by mill.The mill of fiber is pressed or is squeezed The covering surface of chopped fibre simultaneously makes carbon core be exposed to outside, and therefore electric conductivity is improved in part.This will be provided to carbon fiber It contacts and contact is provided between carbon fiber.
This can be by being provided with the rove section for the pultrusion apparatus being defined above for along the multiple fibre One or more equipment of the fiber in Chosen Point are pressed or squeezed to dimension mill to realize.
Such one or more equipment may include rotating wheel and static plate, contact each other to along the multiple fibre Fiber in dimension mill pressure or extruding Chosen Point.
According to an embodiment of the invention, multiple radial directions that rotating wheel includes the rotation axis regular distribution around rotating wheel are dashed forward Portion out, and static plate includes uneven surface, and multiple radially protruding parts and uneven surface are contacted each other to along described Fiber in multiple fiber mill pressures or extruding Chosen Point.
Multiple radially protruding parts can be made of a soft, or alternatively, which can be set flexible support Part.
It present invention can be advantageously used in the slim-lined construction that manufacture will be integrated in wind turbine blade.
It has to be noticed that describing the embodiment of the present invention by reference to different themes.In particular, by reference to device (pultrusion tool and device) class claim describes some embodiments, and describes by reference to method class claim Other embodiments.However, those skilled in the art learn from described above and below, unless otherwise notice, otherwise removes and belong to one Other than any combination of the feature of the theme of seed type, (especially in method class right between feature relevant to different themes It is required that feature and device class claim feature between) any combination be recognized as and disclosed together with this document.
Aspect defined above of the invention and other aspects it is aobvious according to the example for the embodiment that will be described below and It is clear to, and is explained with reference to the example of these embodiments.This hair is described in more detail below with reference to the example of embodiment It is bright, but the example that invention is not limited to these embodiments.
Detailed description of the invention
Fig. 1 shows the schematic layout of a part of the first embodiment of pultrusion apparatus according to the present invention.
Fig. 2 shows the schematic layout of a part of the second embodiment of pultrusion apparatus according to the present invention.
Fig. 3 shows the schematic cross-sectional of the wind turbine including component according to the present invention.
Specific embodiment
Diagram in attached drawing is schematical.It should be noted that in different figures, element similar or identical is accorded with same reference Number.
Fig. 1 shows the first embodiment along longitudinal pultrusion direction X pultrusion apparatus 100 extended.Pultrusion at Type device 100 includes pultrusion die 20, and multiple fibers 110 are pulled through pultrusion die 20 to be immersed in resin In.
Pultrusion die 20 has rectangular cross section.
Pultrusion die 20 is conventional and in pultrusion technique field it is known that and therefore no longer by into one Step detailed description.
With reference to pultrusion direction X, in 20 downstream of pultrusion die, at least the pultrusion item 50 of transport portion forming.
Rove section 80 is set in 20 upstream of pultrusion die with reference to pultrusion direction X.In rove section 80, It collects multiple fibers 110 for example from multiple fiber bobbin (not shown)s and guides it towards pultrusion die 20.
Rove section 80 can be used in 20 upstream of pultrusion die (that is, entering pultrusion die 20 in fiber 110 Change the conduction property of Chosen Point 200 along multiple fibers 110 before).
Can be according to multiple standard selected elements 200, such as it is uniformly distributed along multiple fibers 110.
For this purpose, rove section 80 include one or more nozzle 82(in the embodiment in figure 1, two nozzles 82) with For the drop 60 of conductive adhesive to be injected or deposited at Chosen Point 200 along multiple fibers 110.Nozzle is mounted on multiple phases It answers on arm 83, arm 83 can be according to the mobile Chosen Point to reach multiple fibers 110 of direction Z transverse to pultrusion direction X 200。
According to other embodiments of the invention, arm 83 can move in the plane or on three-dimensional space.
Arm 83 can move above or below multiple fibers 110.
By injecting or depositing the drop 60 of conductive adhesive at Chosen Point 200 along multiple fibers 110, part changes Conduction property at pultrusion item 50.The drop 60 of conductive adhesive provides part connection between adjacent fiber 110, this, which is improved, draws The overall conductivity of extrusion 50.
Fig. 2 shows the second embodiment along longitudinal pultrusion direction X pultrusion apparatus 100 extended.According to Two embodiments are implemented to change along the multiple fiber 110 by changing size or the surface of fiber 110 in Chosen Point 200 Become the conduction property of Chosen Point 200.In particular, can by mill pressure (mash) or squeeze implement change fiber size or Surface.The mill pressure of fiber or the covering surface for squeezing chopped fibre 110, have the conduction property of difference.Removal destroys fiber 110 covering surface makes carbon core be exposed to outside, and therefore the electric conductivity of pultrusion item 50 is improved in part.
For this purpose, in this embodiment, rove section 80 includes around the rotation axis transverse to pultrusion direction X The wheel 85 and static plate 86 of Z rotation.Wheel 85 includes submitting around multiple radially protruding part 87(of rotation axis Z regular distribution Pitch four radially protruding parts 87 of configuration, the regular angular distance being 90 degrees to each other).Radially protruding part 87 is by flexible material system At, such as soft plastic material.Static plate 86 is provided with the uneven rigid surface 88 with multiple discontinuous portions.For example, Surface 88 can be made of sand surface.In rove section 80, fiber 110 passes through between wheel 85 and static plate 86.With one kind Mode selects the mutual distance between wheel 85 and static plate 86 to make, during the rotation that wheel 85 surrounds rotation axis Z, fiber 110 at the Chosen Point 200 periodically pinching between each of radially protruding part 87 and uneven rigid surface 88.Just The scrambling on property surface 88 causes the covering of fiber 110 to rupture, therefore carbon core is made to be exposed to outside.Radially protruding part 87 Flexible material prevents fiber 110 to be broken completely.Alternatively, radially protruding part 87 can be made of stiff materials, and take turns 85 It is provided with elastic supporting member for supporting optical member, pressure and friction between arm and static plate 86 can be limited, this, which has, prevents fiber 110 to be broken Identical purpose.
Fig. 3 shows the wind turbine 1 including component according to the present invention.Wind turbine 1 includes pylon 2, and pylon 2 is pacified On the base portion not being painted.Cabin 3 is arranged on the top of pylon 2.
Wind turbine 1 further includes wind rotor 5, with two, three or more blade 4(Fig. 1 perspective view In, only two blades 4 are visible).Wind rotor 5 can be rotated around rotation axis Y.Blade 4 radially prolongs relative to rotation axis Y It stretches.
Wind rotor 5 is rotatably coupled by means of rotatable shaft 9 with generator 30.
Other possible embodiments (being not shown in attached drawing) according to the present invention, wind rotor 5 and generator 30 directly revolve Turn ground connection (direct drive generator configuration).
The Bearing assembly 8 that is schematically painted is provided to be held in place rotor 5.9 edge of rotatable shaft Rotation axis Y extend.
Blade 4 includes the one or more slim-lined constructions 50 obtained through the invention.

Claims (12)

1. a kind of method of pultrusion item (50) of manufacture for slim-lined construction, the described method comprises the following steps:
It provides pultrusion apparatus (100), includes at least pultrusion die (20), multiple fibers (110) are pulled through The pultrusion die (20) to be immersed in resin,
Change the conduction property of Chosen Point (200) along the multiple fiber (110) in the pultrusion die (20) upstream.
2. the manufacturing method according to claim 1, wherein by injecting or depositing the drop (60) of conductive adhesive come real Apply the conduction property for changing Chosen Point (200) along the multiple fiber (110).
3. the manufacturing method according to claim 1, wherein implemented by changing the size of the fiber (110) along The multiple fiber (110) changes the conduction property of Chosen Point (200).
4. manufacturing method according to claim 3, wherein pressed or squeezed by mill to change size or the surface of fiber.
5. manufacturing method according to claim 3 or 4, wherein remove or destroy the multiple fiber (110) by part At least one of covering surface change the size of fiber.
6. manufacturing method according to any one of the preceding claims, wherein the slim-lined construction is wind turbine A part of blade (4).
7. a kind of for manufacturing the pultrusion apparatus (100) for being used for the pultrusion item (50) of slim-lined construction, described device (100) is extremely It less include: pultrusion die (20), multiple fibers (110) are pulled through the pultrusion die (20) to be immersed in tree In rouge;And rove section (80), the rove section (80) are used in the pultrusion die (20) upstream along described Multiple fibers (110) change the conduction property of Chosen Point (200).
8. pultrusion apparatus (100) according to claim 7, wherein the rove section (80) include for along One or more sprays of the drop (60) of conductive adhesive are injected at Chosen Point (200) or deposited to the multiple fiber (110) Mouth (82).
9. pultrusion apparatus (100) according to claim 7, wherein the rove section (80) include for along The multiple fiber (110) mill pressure or one or more equipment of extrusion fiber (110) in Chosen Point (200).
10. pultrusion apparatus (100) according to claim 9, wherein the rove section (80) includes rotating wheel (85) it contacts each other to static plate (86), the rotating wheel (85) and the static plate (86) along the multiple fiber (110) mill pressure or extrusion fiber (110) in Chosen Point (200).
11. pultrusion apparatus (100) according to claim 10, wherein the rotating wheel (85) includes around described Multiple radially protruding parts (87) of rotation axis (Z) regular distribution of rotating wheel (85), and the static plate (86) includes not Flat surfaces (88), the multiple radially protruding part (87) and the uneven surface (88) are contacted each other to along described more A fiber (110) mill pressure or extrusion fiber (110) in Chosen Point (200).
12. pultrusion apparatus (100) according to claim 11, wherein the multiple radially protruding part (87) is by soft Soft material is made or the wheel (85) is provided with elastic supporting member for supporting optical member.
CN201910414118.1A 2018-05-17 2019-05-17 Pultrusion method and apparatus Active CN110497629B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP18172948.4 2018-05-17
EP18172948.4A EP3569392B1 (en) 2018-05-17 2018-05-17 Pultrusion method and apparatus

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CN110497629A true CN110497629A (en) 2019-11-26
CN110497629B CN110497629B (en) 2021-10-22

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US (1) US11491747B2 (en)
EP (1) EP3569392B1 (en)
CN (1) CN110497629B (en)
DK (1) DK3569392T3 (en)
ES (1) ES2884303T3 (en)

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